Analysis of flow-field in a dual mode ramjet combustor with boundary layer bleed in isolator

Analysis of flow-field in a dual mode ramjet combustor with boundary layer bleed in isolator

A two-dimensional Reynolds averaged Navier Stokes (RANS) simulation of a dual mode ramjet (DMRJ) combustor is performed, modeling the University of Michigan dual-mode combustor experimental setup operating in reacting mode with different equivalence ratios (φ). The simulations are carried out using...

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Bibliographic Details
Main Authors: Nishanth Thillai, Amit Thakur, Srikrishnateja K., Dharani J.
Format: Article
Language:English
Published: KeAi Communications Co., Ltd. 2021-03-01
Series:Propulsion and Power Research
Subjects:
Dual mode ramjet
Scramjet combustor
Shock wave boundary layer interaction
Boundary-layer bleed
Flamelet combustion model
Online Access:http://www.sciencedirect.com/science/article/pii/S2212540X20300614

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http://www.sciencedirect.com/science/article/pii/S2212540X20300614

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